OBJECT AH, 52425 (Decayed)
Orbit data source: Space-Track
Recently launched and/or uncataloged satellites may have evolving metadata. Metadata may include but not limited to: Owner, Maufacturer, Bus, Motor, and Mission.
OBJECT AH, 52425 was a satellite in LEO that was launched on Mon, 02 May 2022 UTC via an ELECTRON launch vehicle from the Rocket Lab Launch Complex (RLLC). Unknown objects in Earth's orbit typically refer to objects detected orbiting the Earth but have not yet been identified or cataloged. These objects could be anything from previously untracked satellites, spent rocket stages, debris from satellite collisions, or even natural meteoroids temporarily captured by Earth's gravity. This object's orbit decayed before it could be identified.
52425 intel report (Beta)
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Edit Public Description
| Identifier | |
| Orbit | Decayed |
| Last TLE update | 7 months ago |
| Origin | |
| Manufacturer | E-Space |
| Mission | Decayed Commercial Communications |
| Bus & Motor | CUBESAT 6U?, Unknown motor |
| Mass | ~10 kg wet, ~10 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Unknown |
| Shape & HBR | Box + 2 Pan, 1 m |
| Radar Cross Section | 0.126 m², Small (<0.1 m²) |
Expand to show TLE details & history
TLE from 7 months ago
0 OBJECT AH
1 52425U 22047AH 24220.38791822 .09950694 25075-5 11309-2 0 9995
2 52425 97.3633 315.2486 0014929 267.1874 92.7715 16.36640179127969Definitive object data (Epoch: 2024-08-07T09:18:36.134Z)
| Latitude | -0.00001° |
| Longitude | -140.79371° |
| Altitude | 178.491 km |
| Speed | 7.799 km/s |
| True Right ascension | 21h 00m 59s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in full shadow at TLE epoch |
Visualization observer readout
| Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed. |
Visualization observer readout
| Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed. |
Orbital elements
| Apogee altitude | 181.344 km |
| Perigee altitude | 161.788 km |
| Semi-major axis | 6,549.703 km |
| Eccentricity | 0.0014929 |
| Inclination | 97.3633° |
| RAAN | 315.2486° |
| Arg. of periapsis | 267.1874° |
| True anomaly | 92.94236° |
| Mean anomaly | 92.7715° |
| Eccentric anomaly | 92.85693° |
| Mean motion | 4.09459 °/min |
| BSTAR | 0.0011309 |
| Orbital period | 87.92 mins |
Other satellites on launch #47 in the year 2022 (2022-05-02 UTC)
OBJECT AH Visibility forecast
Observer location: undefined°, undefined
Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
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